An apparatus is disclosed that includes a gas turbine engine including a first rotor blade axially adjacent a second rotor blade and an aperture formed in one of the first rotor blade and the second rotor blade and structured to emit a fluid therefrom. A fluid source is in flow communication with the aperture and configured to flow the fluid through the aperture.
ROTOR NOISE SUPPRESSION
ROTORRAUSCHUNTERDRÜCKUNG
SUPPRESSION DE BRUIT DE ROTOR
07.11.2018
Patent
Elektronische Ressource
Englisch
Europäisches Patentamt | 2025
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